View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 23839U 26065.15542823 +.00000000 +00000-0 +00000-0 0 00007
2 23839 10.3877 47.5673 0005965 272.0702 268.7565 0.99997842 06
| Epoch (UTC): | 06 March 2026 03:43:48 |
| Eccentricity: | 0.0005965 |
| inclination: | 10.3877° |
| perigee height: | 35838 km |
| apogee height: | 35889 km |
| right ascension of ascending node: | 47.5673° |
| argument of perigee: | 272.0702° |
| revolutions per day: | 0.99997842 |
| mean anomaly at epoch: | 268.7565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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